|Publication number||US6898354 B2|
|Application number||US 10/694,656|
|Publication date||May 24, 2005|
|Filing date||Oct 27, 2003|
|Priority date||Oct 28, 2002|
|Also published as||US20040109650, WO2004040348A1, WO2004040348B1|
|Publication number||10694656, 694656, US 6898354 B2, US 6898354B2, US-B2-6898354, US6898354 B2, US6898354B2|
|Inventors||Young Joon Kim, Francis A. Gnatek, Jeffrey S. Doak|
|Original Assignee||Judd Wire, Inc.|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (29), Referenced by (39), Classifications (8), Legal Events (6)|
|External Links: USPTO, USPTO Assignment, Espacenet|
This application claims priority from U.S. Provisional Patent Application Ser. No. 60/421,665, filed Oct. 28, 2002.
The present invention generally relates to fiber optic cables, and more particularly relates to a fiber optic cable that employs a dual layer jacket demonstrating improved dimensional stability over a wide temperature range. In a preferred embodiment, the inventive cable is flame-retardant and, upon flaming, smoke suppressed and non-hazardous.
Fiber optic cables are currently being used throughout the aerospace and communications industries. These cables are typically employed in computerized equipment and communications applications where space and/or weight restrictions make traditional copper wiring systems inappropriate. Optical fiber, as a data transfer means, is known for its exceptional speed and bandwidth capability and for its ability to provide reliable communication signals in systems that generate large amounts of electromagnetic radiation.
The commercial and military aerospace industry is a harsh testing ground for fiber optic cables, requiring flawless performance in extremely demanding physical environments. In such environments, where even minor failures can result in loss of life and property, fiber optic cables are subjected to conditions which include destructive extremes in vibration, shock, temperature, pressure, water/chemical emersion, as well as electromagnetic and radio frequency interference. It is for these reasons that aerospace standards for the manufacture and supply of fiber optic cables are some of the most rigorous found in any industry.
The world's major aerospace manufacturers conduct aggressive ongoing research on new designs and materials that can deliver stronger, lighter and more durable fiber optic cables.
U.S. Pat. No. 6,233,384 B1 to Sowell, III et al. provides one such new design. By way of this reference, a ruggedized fiber optic cable is provided wherein a fluoropolymer first jacketing material is applied over a buffered optic fiber core. A rigid, closely-spaced, spirally or helically wrapped wire layer is applied over the first jacketing layer, followed by the application of a mechanical braid (e.g., plastic fibers or strands) over the wire layer. To protect the fiber optic cable from the environment, an outer jacket (e.g., tetrafluoroethylene/(perfluoroalkyl) vinyl ether copolymer) is applied over the mechanical braid. Although this cable design provides some protection for the optic fiber core, the outer jacket will shrink in the axial direction during cable manufacture and use, thereby increasing stress on the optic fiber core, which can cause the fibers to crack or break.
U.S. Pat. No. 5,615,293 to Sayegh discloses a fiber optic cable assembly that employs acrylic coated optical fibers surrounded by a buffer material such as foamed fluorinated ethylene-propylene (FEP). The acrylic coating material on the optical fibers, however, has a use temperature ranging from about −65° C. to about 125° C. and will degrade when the FEP buffer material is extruded onto the fibers, causing undesirable yellowing and even loss of integrity of the coating material.
Accordingly, it is a general object of the present invention to avoid the above-referenced disadvantages of the prior art.
More particularly, it is an object of the present invention to provide a fiber optic cable that serves to minimize or eliminate shrinkage stress on the optic fiber core.
It is a more particular object to provide a fiber optic cable having improved dimensional stability that demonstrates more stable signal carrying characteristics in extremely demanding physical environments.
It is another more particular object to provide a fiber optic cable that employs one or more intermediate layers that serve to protect the buffered optical fiber(s) from the effects of high temperature during cable manufacture and use.
The present invention therefore provides a fiber optic cable that comprises:
The present invention further provides a process for preparing the fiber optic cable described above, which comprises:
Other features and advantages of the invention will be apparent to one of ordinary skill from the following detailed description and accompanying drawings.
Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. All publications, patent applications, patents and other references mentioned herein are incorporated by reference in their entirety. In case of conflict, the present specification, including definitions, will control. In addition, the materials, methods, and examples are illustrative only and not intended to be limiting.
Particular features of the disclosed invention are illustrated by reference to the accompanying drawings in which:
By way of the present invention, it has been discovered that improved dimensional stability in fiber optic cables may be achieved using a dual layer jacket comprising a heat or pressure sealed, low shrinkage polymer film inner layer and an outer protective layer. As alluded to above, dimensional stability (e.g., low axial shrinkage) is one of the most important properties of a fiber optic cable.
The fiber optic cable of the present invention was developed primarily for use in aerospace applications and preferred embodiments thereof comply with the flame spread, smoke, toxicity and out-gassing standards of the aerospace industry. Its application, however, is not limited to aerospace applications, and may, if desired, be used in automotive, vehicular, shipboard and industrial applications, and the like.
Referring now to
Optical fibers suitable for use in the present invention are not limited and include glass fibers, plastic or polymer fibers and plastic-clad fibers. Such fibers may take the form of single-mode fibers or multi-mode fibers, with multi-mode fibers being further divided into step-index, multi-mode fibers and graded-index, multi-mode fibers.
A “mode” is defined as a transverse pattern of energy that propagates through an optical fiber at a specific velocity. As the names suggest, single-mode fibers only support a single mode, while multi-mode fibers support a number of modes.
For step-index, multi-mode fibers, the index of refraction (i.e., the ability of a material to bend light) is the same across the entire radius of the fiber core, but sharply decreases at the core/cladding interface. In the case of graded-index, multi-mode fibers, the index of refraction gradually changes across the radius of the core from a maximum at the center to a minimum near the edges.
In one preferred embodiment, optical fiber 12 is a single-mode optical fiber having a core diameter of approximately 9 micrometers (μm) and a cladding diameter of approximately 125 μm.
In another preferred embodiment, optical fiber 12 is a graded-index, multi-mode optical fiber having a core diameter of approximately 62.5 μm and a cladding diameter of approximately 125 μm.
The primary buffer member 14, which is tightly bonded to each optical fiber 12, provides the first layer of mechanical protection to fiber(s) 12 by cushioning and protecting the fiber(s) when the fiber(s) is bent, cabled, or spooled. As is well known to those skilled in the art, stresses placed upon optical fibers during handling may induce microbending of the fibers, resulting in attenuation of the light, which is intended to pass through them, and thus inefficient signal transmission.
Materials suitable for use in preparing primary buffer member 14 include, but are not limited to, silicones, acrylic polymers, acrylates and polyimides.
For example, primary buffer member 14 may be prepared using acrylate functional monomers and/or oligomers in the form of a polymer coating that is applied to the fiber from a melt or a solution of the polymer, or is extruded onto the fiber. Such buffered fibers have a use temperature ranging from about 85° C. to about 125° C. and can degrade when exposed to temperatures that exceed the upper end of this range during cable manufacture and use, causing undesirable yellowing and even loss of integrity of the coating material.
In a preferred embodiment, optical fiber(s) 12 is a graded-index, multi-mode optical fiber that is buffered with acrylate functional monomers and/or oligomers. Such buffered fibers are available from Corning, Inc., 1 Riverfront Plaza, Corning, N.Y. 14831-0001 (“Corning”), OFS Fitel Denmark I/S, Priorparken 680, DK-2605 Brøndby, Denmark (“OFS Fitel”), and Nufern, Inc., 7 Airport Park Road, East Granby, Conn. 06026-9523 (“Nufern”). Corning and OFS Fitel sell these buffered fibers under the trade designations INFINICOR buffered fibers and GIGAGUIDE buffered fibers, respectively.
Primary buffer member 14 may also be prepared using polyimides. Polyimide buffered optical fibers have a use temperature ranging from about 150° C. to about 250° C. and thus do not degrade during normal cable manufacture and/or use.
In another preferred embodiment, optical fiber(s) 12 is a graded-index, multi-mode optical fiber that is buffered with a heat-resistant polyimide. Such buffered fibers are available from OFS Fitel.
In yet another preferred embodiment, optical fiber(s) 12 is a radiation hardened, graded-index, multi-mode optical fiber that is buffered with a polyimide.
Such fibers, which are resistant to gamma (γ-radiation, are available from Nufern.
When a plurality of coated or buffered optical fibers are used, it is s preferred that such fibers take the form of an optical fiber assembly (e.g., ribbon assemblies, cables) to simplify construction and to eliminate the need to handle individual fibers. The fibers in such assemblies are bonded together in a matrix material (e.g., polyester resin), which either encases the fibers or edge-bonds the fibers together. Optical fiber assemblies, comprising single-mode ribbon cables, are available from Sumitomo Electric Lightwave Corp., Sumitomo Electric, 78 TW Alexander Drive, Research Triangle Pa., NC 27709 (“Sumitomo Lightwave”), under the product designation LITEPIPE ribbon cables.
The secondary buffer member 16 provides another layer of mechanical protection to optical fiber 12, preventing damage to the fiber during processing and use. This layer may be formed by either extruding a fluoropolymer material along a portion or length of the primary buffer member 14, or by wrapping a fluoropolymer film, in an overlapping fashion, along a portion or length of member 14.
The secondary buffer member 16 is preferably held tightly against (but not bound to) primary buffer layer 14.
In one embodiment, secondary buffer member 16 is a high-temperature, fluoropolymer buffer member. Fluoropolymers which may advantageously be utilized in the secondary buffer layer 16 of fiber optic cable 10 of the present invention include, for example, FEP, polytetrafluoroethylene-perfluoromethylvinylether (MFA), perfluoroalkoxy (PFA), polytetrafluoroethylene (PTFE), ethylene-chlorotrifluoroethylene (ECTFE) copolymers, ethylene-tetrafluoroethylene (ETFE) copolymers, polyvinylidene fluoride (PVDF), tetrafluoroethylene-hexafluoropropylene-vinylidene fluoride (THV), polyvinylfluoride (PVF) resins, and mixtures thereof.
In a preferred embodiment, secondary buffer member 16 is extruded and the fluoropolymer is either PFA or a copolymer or terpolymer of ETFE. In a more preferred embodiment, the polymer is a high purity, high melt flow, low shrinkage PFA resin. Such resins are available from DuPont under the product designation TEFLON PFA 440 HP-D perfluoroalkoxy resins.
Secondary buffer member 16 preferably has a wall thickness ranging from about 300 μm to about 350 μm and an inner diameter ranging from about 240 μm to about 350 μm.
Strength member 18 serves to bear most of the force imparted to fiber optic cable 10 by e.g. pulling and other mechanical strains. Strength member 18 exhibits little or no elongation and in a preferred embodiment is prepared from reinforcing materials loosely braided, woven or wound, about the exterior of the secondary buffer member 16. In a more preferred embodiment, the reinforcing materials are straight, axially extending yarns or fibers that circumferentially surround secondary buffer member 16 (e.g., a straight, axial lay-up). Materials suitable for use in this layer include metal (e.g., carbon, carbon steel, copper, brass, stainless steel and alloys thereof) and non-metal (e.g., aramid, glass, polyester, polyimide) reinforcing materials.
In a preferred embodiment, strength member 18 is prepared using aramid yarns or fibers. Aramid yarns or fibers are sold by E. I. du Pont de Nemours and Company, 1007 Market Street, Wilmington, Del. 19898 (“DuPont”), under the trade designations KEVLAR synthetic para-aramid fibers and NOMEX synthetic meta-aramid fibers, and by Teijin Shoji (USA), 42 W 39th St. Fl. 6, New York, N.Y. 10018-3809, USA, under the trade designation TECHNORA para-aramid fibers.
In a more preferred embodiment, strength member 18 is prepared using a fiber-reinforced composite or fabric comprising aromatic polyamide fibers in a resinous matrix, to axially extend and circumferentially surround secondary buffer member 16. Such fiber-reinforced composites or fabrics are available from DuPont under the trade designations KEVLAR 29 and KEVLAR 49 aramid fabrics.
In another preferred embodiment, strength member 18 is prepared using either polyimide films or glass fiber-reinforced composites.
Strength member 18 preferably has a wall thickness ranging from about 300 μm to about 330 μm and an inner diameter ranging from about 890 μm to about 910 μm.
The dual layer jacket 20 of the fiber optic cable 10 of the present invention comprises a heat or pressure sealed, low-shrinkage polymer film inner layer 22, and an outer protective layer 24.
The polymer film inner layer 22 of dual layer jacket 20, which is held loosely around strength member 18, demonstrates low axial shrinkage and maintains high bond strength between heat or pressure sealed, overlapping film regions even at high temperatures (i.e., greater than or equal to 200° C.), thus serving to increase the dimensional stability of jacket 20.
Films suitable for use in inner layer 22 are heat or pressure sealable, low-shrinkage polymer films prepared from materials including, but not limited to, fluoropolymers and polyimides.
In one preferred embodiment, the low-shrinkage polymer film is a fluoropolymer film.
In another preferred embodiment, the low-shrinkage polymer film is a polyimide film. Any film-forming polyimide may be used in the practice of the present invention, with preferred polyimides being aromatic polyimide films. In a more preferred embodiment, the polyimide film is a polyimide copolymer film derived from the reaction of an aromatic tetracarboxylic acid dianhydride component comprising from 0 to 95 mole %, preferably from 10 to 95 mole %, of 3,3′,4,4′-biphenyltetracarboxylic dianhydride and from 5 to 100 mole %, preferably from 5 to 90 mole %, of pyromellitic dianhydride, and an aromatic diamine component comprising from 25 to 99 mole %, preferably from 40 to 98 mole %, of p-phenylene diamine and from 1 to 75 mole %, preferably from 2 to 60 mole %, of a diaminodiphenyl ether such as 4,4′-diaminodiphenyl ether, 3,3′-diaminodiphenyl ether or 3,4′-diaminodiphenyl ether. Such films are described in U.S. Pat. No. 5,731,088 to Philip R. La Court, which is incorporated herein by reference.
The polyimide films used in inner layer 22 are films having a sealable component (i.e., a heat-sealable or pressure sensitive adhesive) coated or laminated on/to at least one surface. It is noted that such films are typically purchased with at least one surface coated with a heat-sealable adhesive, where the coating or lamination of such films constitutes a highly specialized area of practice undertaken by only a limited number of companies.
Heat-sealable adhesives, which may be used in the present invention, include perfluoropolymer, crosslinkable fluoropolymer, and polyimide adhesives.
Perfluoropolymer adhesives, appropriate for use in the present invention, include PTFE, FEP, PFA, and copolymers of tetrafluoroethylene and perfluoromethylvinylether (MFA) adhesives, while suitable crosslinkable fluoropolymer adhesives include ETFE and chlorotrifluoroethylene (CTFE) copolymer and terpolymer adhesives which contain minor amounts of one or more fluorinated comonomers (e.g., HFP, HFIB, PFBE, VDF and VF).
Polyimide adhesives, suitable for use in the present invention, include thermoplastic polyimide adhesives, which soften and become fluid at or above 200° C.
Preferred heat-sealable films are polyimide films coated or laminated with a heat-sealable fluoropolymer adhesive. Such materials are available from DuPont, under the trade designations OASIS 120TWT 561 and OASIS 200TRT515 heat-sealable composite films. Most preferred heat-sealable films are polyimide films coated or laminated with a heat-sealable polyimide adhesive. Such materials are also available from DuPont, under the trade designations KAPTON HKJ, KAPTON EKJ, and ELJ heat-sealable polyimide films.
The heat or pressure sealable films are preferably applied to strength member 18 in tape form, by either spirally or axially wrapping the tape about strength member 18.
For spiral-wrap applications, the tape preferably has a width ranging from about 0.3 to about 1 centimeter (cm), and a thickness ranging from about 0.01 to about 0.04 millimeters (mm). The tape is preferably wrapped so as to achieve a degree of overlap ranging from about 15 to about 70%.
In regard to axial-wrap applications, the tape preferably has a width ranging from about 0.5 to about 1 cm, and a thickness ranging from about 0.01 to about 0.04 mm. For much larger cable applications, such as multiplex cable applications, the tape preferably has a width of from about 110 to about 150% of the cable circumference, and a thickness ranging from about 0.01 to about 0.04 mm. The polyimide tape is preferably wrapped so as to achieve a degree of overlap ranging from about 10 to about 30%.
After a heat-sealable tape is applied to strength member 18, the resulting assembly may be heated (in a separate heating step) to a temperature ranging from about 240 to about 350° C., preferably from about 300 to about 320° C. The purpose of the heating operation is to bond or fuse the overlapping regions of the tape, thereby forming an effective seal against moisture along the length of the inner layer 22. As will be readily apparent to those skilled in the art, such a separate heating step may be unnecessary if the assembly will be exposed to such temperatures during the extrusion of outer layer 24.
The polymer film inner layer 22 exhibits low shrinkage, thereby maintaining the seal and minimizing stress to the optical fibers, which can cause the fibers to crack or break. The term “low shrinkage,” as used herein, is intended to mean an axial shrinkage of less than or equal to 0.5%.
The wall thickness of inner layer 22 preferably ranges from about 0.02 mm to about 0.5 mm, while its inner diameter preferably ranges from about 1.4 mm to about 1.8 mm.
Inner layer 22 demonstrates a high temperature (i.e., 150° C.) adhesive bond strength ranging from about 100 to about 250 grams per inch-width (gm/inch-width). When inner layer 22 is prepared using a polyimide film coated or laminated with a heat-sealable polyimide adhesive, it demonstrates a high temperature (i.e., 150° C.) adhesive bond strength of greater than 1000 gm/inch-width, preferably greater than 1500 gm/inch-width. High temperature adhesive bond strength is measured in accordance with ASTM# 1876-00—Standard Test Method for Peel Resistance of Adhesives (T-Peel Test).
The high degree of high temperature adhesive bond strength demonstrated by inner layer 22, when prepared using the preferred heat-sealable films, has been found to be particularly surprising.
Outer protective layer 24 of dual layer jacket 20 serves to protect fiber optic cable 10 from the environment and in a preferred embodiment, to provide cable with flame retardant properties.
Outer layer 24 is preferably prepared using a fluoropolymer material. Fluoropolymers which may advantageously be utilized in layer 24 include, for example, polytetrafluoroethylene-perfluoromethylvinylether (MFA), perfluoroalkoxy (PFA), polytetrafluoroethylene (PTFE), ethylene-chlorotrifluoroethylene (ECTFE) copolymers, ethylene-tetrafluoroethylene (ETFE) copolymers, fluorinated ethylene-propylene (FEP), polyvinylidene fluoride (PVDF), tetrafluoroethylene-hexafluoropropylene-vinylidene fluoride (THV), polyvinylfluoride (PVF) resins, and mixtures thereof.
In a more preferred embodiment, the fluoropolymer of outer protective layer 24 is a PFA fluoropolymer.
The fluoropolymer(s) preferably contains a photosensitive substance (e.g., titanium dioxide), which renders the outer protective layer 24 receptive to laser marking. The term “laser marking,” as used herein, is intended to mean a method of marking a fiber optic cable using an intense source of ultraviolet or visible radiation, preferably a laser source. In accordance with this method, exposure of the outer protective layer 24 to such intense radiation will result in a darkening where the radiation was incident. By controlling the pattern of incidence, marks such as letters and numbers can be formed. In a more preferred embodiment, the fluoropolymer(s) contains (as extruded) from about 1 to about 4% by weight, of titanium dioxide.
In addition to the above component, the fluoropolymer(s) may advantageously contain other additives such as antioxidants, crosslinking agents (e.g., triallyl isocyanurate (TAIC), triallylcyanurate (TAC) and trimethallylisocyanurate (TMAIC)), dyes, fibers, lubricants (e.g., PTFE powder), mineral fibers, pigments (e.g., titanium oxide), plasticizers, stabilizers, and the like. However, some such additives may have an adverse effect on the desirable properties of the fiber optic cable 10 of the present invention.
When outer protective layer 24 is prepared using a non-fluoropolymer material, the non-fluoropolymer material preferably contains (as extruded) from about 15 to about 40% by weight of a flame-retarding agent. Suitable flame-retarding agents include aluminum trihydrate, clay, magnesium carbonate, metal hydroxides (e.g., aluminum hydroxide, magnesium hydroxide), talc, and mixtures thereof. In a more preferred embodiment, the flame-retarding agent is magnesium hydroxide, which is available from Kyowa Chemical Industry Co., Ltd., Sakaide, Kagawa 762-0012, Japan, under the product designation KISUMA 5.
Outer layer 24 may be formed by either extruding a fluoropolymer or non-fluoropolymer material along a portion or length of inner layer 22, or by wrapping a fluoropolymer or non-fluoropolymer film, in an overlapping fashion, along a portion or length of layer 22. In a preferred embodiment, outer layer 24 is formed by melt-kneading and extruding a fluoropolymer material onto inner layer 22 using a twin-screw extruder.
Fiber optic cable 10 may be subjected to a so-called “skin irradiation” process to effect crosslinking in the outer protective layer 24. The subject process employs ionizing radiation in the form of accelerated electrons, and basically comprises using an accelerated voltage such that the maximum attained distance of accelerated charged particles is less than or equal to the thickness of the outer layer 24. More specifically, with an applied voltage of 120 KV, most electrons will penetrate outer layer 24 to a maximum depth of approximately 0.20 mm.
The present inventors have found that such a “skin irradiation” process will not serve to damage the optical fiber(s) 12 or the primary buffer member 14.
Such a technique or process is briefly described in JP 4-52570 in regard to automotive low voltage wire coated with e.g. a soft vinyl chloride resin. JP 4-52570 is incorporated herein by reference.
Outer layer 24 of dual layer jacket 20 preferably has a wall thickness ranging from about 0.08 mm to about 0.25 mm, and an inner diameter ranging from about 1.5 mm to about 2.0 mm.
In a more preferred embodiment of the present invention, fiber optic cable 10 comprises:
In yet a more preferred embodiment, fiber optic cable 10 of the present invention further comprises a heat insulating and dimensionally stabilizing member 26. Member 26 is located between the primary and secondary buffer members 14, 16, circumferentially surrounding primary buffer member 14. As its name implies, member 26 performs two functions. First, it serves to insulate the primary buffer member 14 from high processing temperatures used during cable manufacture. For example, when the secondary buffer member 16 is prepared using a high temperature fluoropolymer, temperatures of 350° C. or higher may be used to extrude this material over the primary buffer member 14. As will be readily evident to those skilled in the art, member 26, due to its heat insulating function, allows for the use of a wide variety of primary buffer materials including those materials that may degrade at such high processing temperatures (e.g., acrylates). Second, the heat insulating and dimensionally stabilizing member 26, which is tightly braided, woven or wound about (but not bound to) the exterior of primary buffer member 14, also serves to stiffen and reduce shrinkage of the primary buffer member 14.
In this more preferred embodiment, secondary buffer member 16 is bonded to, or embedded in, heat insulating and dimensionally stabilizing member 26, whereby member 26 also serves to reduce shrinkage in the secondary buffer member 16. Bonding or embedment may be achieved by e.g. extruding the fluoropolymer material of secondary buffer member 16 under vacuum along a portion or length of member 26.
Materials suitable for use in this layer exhibit little or no elongation and include non-metal, heat insulating materials such as aramids, glass, polyesters and polyimides.
In one preferred embodiment, the heat insulating and dimensionally stabilizing member 26 is formed by spirally or cigarette wrapping an aramid paper tape (e.g., NOMEX aramid paper tape), in an overlapping fashion, along a portion or length of the primary buffer member 14.
In another preferred embodiment, the heat insulating and dimensionally stabilizing member 26 is prepared using aramid yarns or fibers. For example, when optical fiber assemblies are employed, member 26 may be prepared by spiral wrapping an aromatic polyamide fiber-reinforced polymer composite or fabric, which comprises helically orientated, aromatic polyamide fibers fixed in a resinous matrix, around the primary buffer member 14. Such fiber reinforced polymer composites are available from DuPont under the trade designations KEVLAR 29 and KEVLAR 49 aramid fabrics.
Heat insulating and dimensionally stabilizing member 26 preferably has a wall thickness ranging from about 0.15 mm to about 0.25 mm and an inner diameter ranging from about 0.24 to about 0.35 mm.
In a most preferred embodiment of the present invention, and as best shown in
The process for preparing fiber optic cable 10 basically comprises:
When the inventive process includes the step of crosslinking the outer protective layer 24, the process may further comprise the step of subjecting the fiber optic cable 10 to thermal treatments to eliminate or further reduce shrinkage in the secondary buffer member 16 and in the outer layer 24 of dual layer jacket 20.
During installation of the inventive fiber optic cable 10, staggered portions of the dual layer jacket 20 (e.g., about 35 mm), the strength member 18 (e.g., about 27 mm), the secondary buffer member 16 (e.g., about 20 mm), and the primary buffer member 14 (e.g., about 13 mm), may be removed to expose a predetermined length of the optical fiber(s) 12. Thereafter, the optical fiber(s) 12 may be bonded to a ferrule followed by the positioning of a connector (e.g., crimp collar) over the exposed portion of the strength member 18. The connector may be mechanically attached to cable 10 by applying sufficient force to deform the connector around the strength member 18 and to effect a seal between the inside surface of the connector and the exposed surface of member 18.
The fiber optic cable 10 of the present invention, which demonstrates improved dimensional stability, has more stable signal carrying characteristics under severe conditions. In other words, the inventive cable 10 minimizes or removes stress when cable 10 is bent or heat cycles on use.
Preliminary testing of a more preferred embodiment of the present invention and a cable employing a single layer jacket has confirmed, as set forth in Table 1 below, that the fiber optic cable of the present invention demonstrates improved dimensional stability in the form of reduced jacket shrinkage and thus reduced optical attenuation in the cable.
Dimensional stability was measured by first exposing the fiber optic cable to a temperature cycling regimen (i.e., temperatures ranging from about −65° C. to about 180° C. for polyimide buffered fibers, temperatures ranging from about −65° C. to about 135° C. for acrylate buffered fibers) using a dynamic mechanical analyzer (DMA) with zero load and measuring jacket shrinkage in accordance with the test procedures detailed in Boeing Standard BMS 13-71 entitled “Draft BMS 13-71 Cable, Fiber Optic” dated Mar. 23, 2002 (“Boeing BMS 13-71”), and in Judd Wire, Inc.'s Standard Operating Procedure (SOP) Number 90111, entitled “Shrinkage Measurement Method”, anticipated publication date—Oct. 29, 2003 (“judd SOP 90111”), and then by measuring the stability of optical attenuation in the cable in accordance with the test procedure detailed in Electronic Industries Association (EIA)/Telecommunications Industry Association (TIA) Test Procedure Number 455-3A, dated May 23, 1989 (“EIA/TIA Test Procedure Number 455-3A”), said test procedures being incorporated herein by reference. The results are shown in Table 1, below.
Summary of Example 1 and Comparative Example C-1
Optical fiber coated
62.5/125 μm graded-
with primary buffer
optical fiber buffered
with a heat-resistant
Dual layer jacket
sealable polyimide film4
Single layer jacket
Jacket shrinkage5 (%)
Attenuation of the
Too high to measure
1manufactured by OFS Fitel under the trade designation Optical Fiber with Polyimide Primary Buffer.
2manufactured by DuPont under the trade designation TEFLON PFA 440 HP- D perfluoroalkoxy resins.
3manufactured by DuPont under the trade designation KEVLAR 49 aramid fabrics.
4manufactured by DuPont under the trade designation KAPTON ELJ heat-sealable polyimide films.
5Judd SOP 90111.
6EIA/TIA Test Procedure Number 455- 3A.
The results shown in Table 1, demonstrate that when the optical fiber is a 62.5/125 μm graded-index, multi-mode optical fiber, the inventive fiber optic cable (Example 1) demonstrates an optical attenuation of about 2.3 decibels per kilometer (dB/km) at 1300 nanometers (nm), which is dramatically less than the optical attenuation demonstrated by a similar cable jacketed with a single layer of extruded PFA (Example C-1).
More preferred optical attenuations for the inventive fiber optic cables employing one or more 62.5/125 μm graded-index, multi-mode optical fibers, will be less than about 3.0 dB/km at 1300 nm (most preferably, less than about 2.0 dB/km at 1300 nm), while fiber optic cables employing one or more 9/125 μm single-mode optical fibers, will demonstrate an optical attenuation of less than about 2.5 dB/km at 1300 nm (most preferably, less than about 1.5 dB/km at 1300 nm), when tested in accordance with EIA/TIA Test Procedure Number 455-3A.
In addition, inventive fiber optic cable 10 satisfies aerospace industry standards for flame spread and smoke generation, toxicity and out-gassing. More specifically, the inventive cable meets or exceeds the requirements of Boeing BMS 13-71.
While various embodiments of the present invention have been described above, it should be understood that they have been presented by way of example only, and not limitation. Thus, the breadth and scope of the present invention should not be limited by any of the exemplary embodiments.
Having thus described the invention, what is claimed is:
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|Cooperative Classification||G02B6/4483, G02B6/4402, G02B6/4433, G02B6/4436|
|European Classification||G02B6/44C7A1L, G02B6/44C9F|
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|Feb 24, 2009||SULP||Surcharge for late payment|
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Year of fee payment: 4
|Jan 7, 2013||REMI||Maintenance fee reminder mailed|
|May 24, 2013||LAPS||Lapse for failure to pay maintenance fees|
|Jul 16, 2013||FP||Expired due to failure to pay maintenance fee|
Effective date: 20130524